According to the present invention, when a de-orbiting satellite, which is one among artificial satellites belonging to a first satellite constellation (101), de-orbits from an orbit of a first orbital altitude band and descends, a second satellite constellation (102) creates an empty orbital region in a second orbital altitude band by expanding the relative angle of any two neighboring orbital planes among a plurality of orbital planes. The de-orbiting satellite passes through the empty orbital region of the second orbital altitude band.


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    Titel :

    Satellite constellation maintenance method, satellite constellation, orbit descent method, and artificial satellite


    Beteiligte:
    HISAYUKI MUKAE (Autor:in)

    Erscheinungsdatum :

    2024-04-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS